View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58465U 26145.61818993 +.00000000 +00000-0 +89152-3 0 00002
2 58465 97.3356 233.0098 0007043 217.3487 142.7300 15.93839434 00
| Epoch (UTC): | 25 May 2026 14:50:11 |
| Eccentricity: | 0.0007043 |
| inclination: | 97.3356° |
| perigee height: | 287 km |
| apogee height: | 296 km |
| right ascension of ascending node: | 233.0098° |
| argument of perigee: | 217.3487° |
| revolutions per day: | 15.93839434 |
| mean anomaly at epoch: | 142.7300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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